b) Each Engine shall have completed a maximum power assurance run in accordance with the engine manufacturer's maintenance manual and any discrepancy noted that exceed the applicable Manufacturer's Maintenance Manual limits shall be corrected by Lessee. In addition, each Engine will operate within the green band with respect to the Engine EGT.



 c) No Engine shall be on "Watch" for any adverse trends that indicate deterioration in the performance of the Engine or as concluded from the review of engine condition monitoring records during the last three (3) months of the Term.



 d) An inspection of the Engine's filters and magnetic chip detectors shall also be accomplished by Lessor to determine any adverse indications.



80. FUSELAGE, WINDOWS AND DOORS:


 a) Fuselage shall be free of major dents and abrasions, time limited patches and loose or pulled or missing rivets. All sheet metal and structural repairs shall be in compliance with the applicable manufacturer's structural repair manual or alternatively as approved and documented by the FAA and unless existing and documented on the Commencement Date, shall be permanent in nature. Repair and dent mapping shall be accomplished at the redelivery "C" check prior to redelivery to Lessor;



 b) Doors shall be free moving, correctly rigged and be fitted with serviceable seals.



94. WINGS AND EMPENNAGE AND ENGINE NACELLES:


 a) All leading edges and control surfaces shall be free from delamination and corrosion which exceeds the Manufacturer's structural repair manual or Manufacturer's approved data, or FAA approved data.



 b) Alll Engine nacelles shall be free of damage which exceeds the applicable Manufacturer maintenance manual limits;



 c) Wings shall be free of fuel leaks.



112. COCKPIT:






 a) All decals shall be clean, secure and legible.